View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65365U 26145.45492199 +.00000000 +00000-0 +45105-3 0 00007
2 65365 53.1586 171.9435 0001163 74.7856 285.3273 15.30205140 04
| Epoch (UTC): | 25 May 2026 10:55:05 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.9435° |
| argument of perigee: | 74.7856° |
| revolutions per day: | 15.30205140 |
| mean anomaly at epoch: | 285.3273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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